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fileTsAGI Science Journal

TsAGI Science Journal
  • PDF2009 Volume 401TsAGI4001 (1-7) Celebrating the Ninetieth Anniversary of the Central Aerohydrodynamic Institute.pdf189.50KB
  • PDF2009 Volume 401TsAGI4001 (103-115) INVESTIGATION OF FLOW SEPARATION PROPAGATION ON PROPELLER BLADES BY THE TUFTS AND LIGHT SHEET TECHNIQUES.pdf2.28MB
  • PDF2009 Volume 401TsAGI4001 (117-129) METHOD OF TAKE-OFF MONITORING BY MEANS OF EFFECTIVE TAKE-OFF SS FUNCTION.pdf886.07KB
  • PDF2009 Volume 401TsAGI4001 (23-37) THE STABILITY OF LAMINAR BOUNDARY LAYER ONTHEPLATE UNDER ELECTROHYDRODYNAMIC ACTION.pdf2.22MB
  • PDF2009 Volume 401TsAGI4001 (39-57) THE EFFECTOFVORTEX WAKE FROM IN ROTOR ONNEAR FIELD SPEED PARAMETERS.pdf3.31MB
  • PDF2009 Volume 401TsAGI4001 (59-72) ANEWMETHODOFBOUNDARY CONDITIONSSTATEMENTAT THEREMOTE BOUNDARY FOR USE IN FINITE-VOLUME METHODSOFNUMERICALSOLUTIONS OF AERODYNAMIC PROBLEMS.pdf1.31MB
  • PDF2009 Volume 401TsAGI4001 (73-85) SELF-SUSTAINED OSCILLATIONS IN A CITY OF A CLOSED CHANNEL DIRECTED TOWARD AN INCIDENT FLOW.pdf3.82MB
  • PDF2009 Volume 401TsAGI4001 (87-101) A PLATE SOUND RADIATION, RELATED WITH ITS INERTIAL BEHIOR IN A NONUNIFORM FIELD OF PRESSURE FLUCTUATIONS.pdf3.92MB
  • PDF2009 Volume 401TsAGI4001 (9-21) APPLICATION OF TANGENTIAL JET BLOWING FOR REDUCTION OF DRAG FOR SUPERCRITICAL AIRFOILS AT HIGH SUBSONIC SPEEDS.pdf4.63MB
  • PDF2009 Volume 402TsAGI4002 (131-149) NUMERICAL SIMULATION OF AERODYNAMICS OF WINGED RE-ENTRY SPACE VEHICLE.pdf1014.26KB
  • PDF2009 Volume 402TsAGI4002 (151-165) OPTIMIZATION OF THE WING SHAPE IN THE WING-BODY SYSTEM AT HYPERSONIC FLOW.pdf706.31KB
  • PDF2009 Volume 402TsAGI4002 (167-190) KINETIC FOUNDATIONS OF THE RANQUE EFFECT MECHANI—HEAT SEPARATION OF FLUID AND GAS FLOW IN A VORTEX TUBE.pdf874.84KB
  • PDF2009 Volume 402TsAGI4002 (191-205) FINITE SYMMETRIC DISTURBANCES PROPAGATION IN A VORTEX CORD.pdf455.99KB
  • PDF2009 Volume 402TsAGI4002 (207-216) PARAMETRIC INVESTIGATIONS OF THE EFFECT OF ICING ON THE AERODYNAMIC CHARACTERISTICS OF A WING AIRFOIL.pdf568.75KB
  • PDF2009 Volume 402TsAGI4002 (217-239) EXPERIMENTAL INVESTIGATION OF AERODYNAMIC LOADS IN THE TIP SECTIONS OF A RIGID BLADE OF AN INCLINED MODEL ROTOR.pdf2.41MB
  • PDF2009 Volume 402TsAGI4002 (241-253) DEVELOPMENT OF A MEASURING TECHNIQUE FOR THE LOW-WENUMBER COMPONENTS OF THE WAVENUMBER-FREQUENCY SPECTRUM OF TURBULENT WALL PRESSURE FLUCTUATIONS.pdf334.77KB
  • PDF2009 Volume 402TsAGI4002 (255-263) INVESTIGATION OF THE FLOW PATTERN NEAR THE PROPELLER IN THE SHAPED RING AND WITHOUT IT AT THRUST REVERSAL.pdf2.11MB
  • PDF2009 Volume 402TsAGI4002 (265-278) THE PRINCIPAL REGULARITIES IN ELASTIC SYSTEM VIBRATIONS AT NONUNIFORM AEROACOUSTIC EXCITATION.pdf340.86KB
  • PDF2009 Volume 403TsAGI4003 (279-298) DEVELOPMENT OF AEROSHAPE AND INVESTIGATION OF ALL-SIZED WINGED RE-ENTRY VEHICLE AEROTHERMODYNAMIC CHARACTERISTICS.pdf599.53KB
  • PDF2009 Volume 403TsAGI4003 (299-307) COMPUTATION OF ICE SHAPES ON AN AIRFOIL.pdf611.33KB
  • PDF2009 Volume 403TsAGI4003 (309-319) EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF BOUNDARY LAYER TRANSITION ON BLUNTED CONES AT SUPERSONIC FLOW.pdf517.35KB
  • PDF2009 Volume 403TsAGI4003 (321-331) COMPUTATIONAL ANALYSIS OF THE EFFICIENCY OF A PROPELLER IN A VISCOUS WAKE USING NIER-STOKES EQUATIONS.pdf432.02KB
  • PDF2009 Volume 403TsAGI4003 (333-353) METHOD FOR DETERMINATION OF AXIAL COMPRESSOR PARAMETERS AT THE BASIC POINTS OF STALLING BRANCH CHARACTERISTICS.pdf700.21KB
  • PDF2009 Volume 403TsAGI4003 (355-365) THE APPROXITION OF THE STANDARD ATMOSPHERE MODEL.pdf507.05KB
  • PDF2009 Volume 403TsAGI4003 (367-378) VIBRATIONS AND ACOUSTIC RADIATION OF THIN-WALLED STRUCTURES AT NONUNIFORM AEROACOUSTIC EXCITATION.pdf581.46KB
  • PDF2009 Volume 403TsAGI4003 (379-391) ROPE SYSTEM PARAMETRIC CONFIGURATION FOR AIRCRAFT TOWING WITH GUARANTEED VERTICAL SHIFT RANGE.pdf438.37KB
  • PDF2009 Volume 403TsAGI4003 (393-399) DESIGN OF A MULTIPURPOSE AEROELASTIC MODULAR MODEL.pdf377.94KB
  • PDF2009 Volume 404TsAGI4004 (401-417) SEVERAL ASPECTS OF GAS FLOW WITH PRESCRIBED DISTRIBUTION OF HEAT SOURCES.pdf145.49KB
  • PDF2009 Volume 404TsAGI4004 (419-436) MONOTONIZATION OF THE FINITE ELEMENT METHOD IN THE PROBLEMS OF GAS DYNAMICS.pdf1.18MB
  • PDF2009 Volume 404TsAGI4004 (437-452) AERODYNAMIC CHARACTERISTICS OF MODELS OF VERTICAL TAKE-OFF AIRCRAFT (TILTROTOR) FOR A WIDE RANGE OF ANGLESOF ATTACK.pdf2.55MB
  • PDF2009 Volume 404TsAGI4004 (459-473) ANALYSIS OF THE SONIC BOOM INTENSITY USING NEAR-FIELD PERTURBATION UNDER THE AIRCRAFT, CALCULATED BY MEANS OF THE NONLINEAR THEORY.pdf618.39KB
  • PDF2009 Volume 404TsAGI4004 (475-483) NUMERIC INVESTIGATION OF THE VENTILATION SYSTEM OF AN ADVANCED AIRCRAFT PASSENGER CABIN.pdf2.00MB
  • PDF2009 Volume 404TsAGI4004 (485-495) A METHOD FOR TAKING INTO ACCOUNT THE INFLUENCE OF THE MODEL AND DYNAMOMETER WEIGHTS ON THE STRAIN-GAUGE BALANCE READINGS.pdf1.24MB
  • PDF2009 Volume 404TsAGI4004 (497-506) APPLICATION OF SIMILARITY TRANSFORTION UPON PARAMETRIC INVESTIGATIONS OF FLUTTER.pdf1.45MB
  • PDF2009 Volume 404TsAGI4004 (507-516) AN ENGINEERING METHOD FOR DETERMINING CHARACTERISTICS OF A PROTECTIVE SCREEN AT IMPACT OF A NONLOCALIZED ENGINE FRAGMENT.pdf4.82MB
  • PDF2009 Volume 405TsAGI4005 (517-534) STUDY OF AERODYNAMICS OF THE AEROSPACE VEHICLE WITH A DEFLECTED BALANCING FLAP.pdf766.92KB
  • PDF2009 Volume 405TsAGI4005 (535-551) LIFT AND INDUCED DRAG OF A FINITE-SPAN WING IN A FLOW OF VISCOUS COMPRESSIBLE GAS AT SUBSONIC SPEEDS.pdf216.28KB
  • PDF2009 Volume 405TsAGI4005 (553-560) ON THE UNSTEADY FLUID FLOWS IN DOINS WITH CLOSED STREAMLINES.pdf143.68KB
  • PDF2009 Volume 405TsAGI4005 (561-569) NOSE PARTS OF MINIL WE DRAG WITH THE FRONT FACE AND THE POWER-LAW GENEATRIX.pdf550.18KB
  • PDF2009 Volume 405TsAGI4005 (571-585) COMPARISON OFTHE RESULTS OF NUMERICAL CALCULATIONS BY THE METHOD BASED ON THE GODUNOV-KOLGAN-RODIONOV DIFFERENCE SCHEME WITH THE EXPERIMENTAL DATA FOR THE TRANSONIC FLOW AROUND RAE 2822 AIRFOIL.pdf2.50MB
  • PDF2009 Volume 405TsAGI4005 (587-607) ABOUT THE SECONDARY SEPARATION AT SUPERSONIC FLOW OVER A COMPRESSION RAMP.pdf1.46MB
  • PDF2009 Volume 405TsAGI4005 (609-617) STUDY OF VISCOUS−INVISCID INTERACTION ON AN OSCILLATING MODEL OF AN AIRPLANE WITH A SWEPT WING.pdf1.16MB
  • PDF2009 Volume 405TsAGI4005 (619-629) RESEARCH ON THERL DYNAMICS OF STRAIN-GAUGE BALANCE AND DEVELOPMENT OF METHODS FOR ITS TEMPERATURE ERROR REDUCTION.pdf2.48MB
  • PDF2009 Volume 405TsAGI4005 (631-0) COMPOUND TRIANGULAR FINITE ELEMENT WITH CUBIC POLYNOMIAL FOR LATERAL PLATE BENDING.pdf811.67KB
  • PDF2009 Volume 406TsAGI4006 (5-656) APPLICATION OF A NEW THEMATICAL TOOL (1D SPECTRAL PORTRAITS OF MATRICES) TO THE PROBLEM OF AEROELASTICITY VIBRATIONS OF TURBINE BLADE CASCADES.pdf1.90MB
  • PDF2009 Volume 406TsAGI4006 (657-667) INVESTIGATION OF THE BPR ENGINE NOZZLE WITH CONTROLLABLE CHEVRONS.pdf681.28KB
  • PDF2009 Volume 406TsAGI4006 (669-682) ASSYMETRY AND NONUNIQUENESS OF THE SOLUTION OF THE PROBLEM OF SEPARATED FLOW OVER A SLENDER CONICAL WING-BODY COMBINATION.pdf819.20KB
  • PDF2009 Volume 406TsAGI4006 (683-694) SUPERSONIC FLOW OVER SHARP ELLIPTICAL CONES.pdf324.80KB
  • PDF2009 Volume 406TsAGI4006 (695-718) PECULIARITIES OF DGM APPLICATION FOR SOLUTION OF 3D EULER AND NIER-STOKES EQUATIONS ON UNSTRUCTURED HEXAHEDRAL GRIDS.pdf771.83KB
  • PDF2009 Volume 406TsAGI4006 (719-732) INVESTIGATION OF THE APPLICATION OF ELECTRICAL DISCHARGES FOR WE DRAG REDUCTION.pdf866.85KB
  • PDF2009 Volume 406TsAGI4006 (733-742) INVESTIGATION OF THE SONIC BOOM OF THE OBLIQUE WING AIRCRAFT.pdf574.97KB
  • PDF2009 Volume 406TsAGI4006 (743-762) MOLECULAR-KINETIC DESCRIPTION OF BROWNIAN MOTION OF HEATED NONSPHERICAL PARTICLES IN HIGHLY RAREFIED GAS.pdf181.33KB
  • PDF2009 Volume 406TsAGI4006 (763-773) EXPERIMENTAL STUDY OF THE JET FLOW CONTROL IN A VEHICLE AFTBODY.pdf1.25MB
  • PDF2010 Volume 411TsAGI4101 (109-118) VIBROACOUSTIC PROCESSES MODELING IN THE TURBOJET ENGINE AND OTHER POWER PLANT UNITS BASED ON FREQUENCY CHARACTERISTICS INVESTIGATION OF THE ENGINE-MOUNTING-AIRFRAME SYSTEM.pdf763.23KB
  • PDF2010 Volume 411TsAGI4101 (15-33) METHOD OF ENGINEERING CALCULATIONS OF ACOUSTIC AND THRUST CHARACTERISTICS OF SE-SUPPRESSING NOZZLES.pdf1.42MB
  • PDF2010 Volume 411TsAGI4101 (3-13) AZIMUTHAL COMPONENTS OF TURBULENT JET SOUND FIELD - MEASUREMENT RESULTS AND THEIR IMPLEMENTATION FOR VALIDATION OFMODERN SE COMPUTATION TECHNIQUES.pdf1.68MB
  • PDF2010 Volume 411TsAGI4101 (35-45) THE TECHNIQUE OF ACCURACY INCREASE WHILE SIMULATING ACOUSTIC DISTURBANCE TRANSFER ON UNSTRUCTURED GRIDS.pdf256.19KB
  • PDF2010 Volume 411TsAGI4101 (47-57) NUMERICAL INVESTIGATION OF THE INTERACTION OF ACOUSTIC DISTURBANCES WITH A SHOCK WE.pdf299.39KB
  • PDF2010 Volume 411TsAGI4101 (59-70) GENERALIZATION OF THE GODUNOV METHOD TO THE PROBLEMS OF COMPUTATIONAL AEROACOUSTICS.pdf384.03KB
  • PDF2010 Volume 411TsAGI4101 (71-78) APPROACH TO THE SOLUTION OF THE INVERSE PROBLEMS OF TURBO-CHINE ACOUSTICS.pdf304.57KB
  • PDF2010 Volume 411TsAGI4101 (79-95) USE OF ACOUSTIC ANALOGY WITH LARGE EDDY SIMULATION FOR TURBULENT JET SE MODELING.pdf1.48MB
  • PDF2010 Volume 411TsAGI4101 (97-107) CORONA DISCHARGE MICROJETS AS POSSIBLE ACTUATORS FOR JET SE CONTROL.pdf1.27MB
  • PDF2010 Volume 412TsAGI4102 (121-131) THREE-DIMENSIONAL ACOUSTIC ANALYSIS WHILE DESIGNING AN AIRCRAFT ENGINE.pdf736.80KB
  • PDF2010 Volume 412TsAGI4102 (133-145) INVESTIGATION OF ACOUSTIC FLUCTUATIONS IN A FLOW WITH PERMEABLE BOUNDARIES USING HOT-WIRE ANEMOMETRY.pdf928.04KB
  • PDF2010 Volume 412TsAGI4102 (147-155) ROLE OF WE DISTURBANCES IN TRANSONIC SEPARATED FLOWS.pdf1.84MB
  • PDF2010 Volume 412TsAGI4102 (157-165) THEMATICAL SIMULATION OF THERMOACOUSTIC CONVECTION ON A PARALLEL SUPERCOMPUTER.pdf364.49KB
  • PDF2010 Volume 412TsAGI4102 (167-175) SUPPRESSION OF PULSATIONS GENERATED BY EXTERNAL ACOUSTIC WES IN A HYPERSONIC SHOCK LAYER.pdf377.05KB
  • PDF2010 Volume 412TsAGI4102 (177-185) ON THE REALIZATION OF A NUMERICAL METHOD THAT PRESERVES THE DISPERSION RELATION ON A DICHOTOMOUS GRID.pdf832.19KB
  • PDF2010 Volume 412TsAGI4102 (187-205) INVESTIGATION OF SUPERSONIC NONISOBARIC JET STRUCTURE.pdf1.34MB
  • PDF2010 Volume 412TsAGI4102 (207-215) SIMULATION OF SELF-OSCILLATORY INTERACTION OF THE SONIC UNDEREXPANDED JET WITH AN OBSTACLE.pdf333.42KB
  • PDF2010 Volume 412TsAGI4102 (217-225) THE PROBLEMS OF MODERN SUPERCOMPUTER APPLICATIONS IN HYDRODYNAMIC AND AEROACOUSTIC NUMERICAL SIMULATIONS.pdf585.18KB
  • PDF2010 Volume 413TsAGI4103 (227-257) PECULIARITIES OF FLOWAND HEAT TRANSFER IN THE BASE AREA OF INTERPLANETARY PROBES.pdf1.11MB
  • PDF2010 Volume 413TsAGI4103 (259-267) THE FUNDAMENTAL PROPERTIES OF SEPARATION IN UNSTEADY SUPERSONIC IDEAL GAS FLOWS.pdf390.30KB
  • PDF2010 Volume 413TsAGI4103 (269-284) NUMERICAL SIMULATION OF THE EFFECT OF ACOUSTICWE INCLINATION ANGLE ON A HYPERSONIC BOUNDARY-LAYER RECEPTIVITY.pdf758.44KB
  • PDF2010 Volume 413TsAGI4103 (285-299) SURFACE TEMPERATURE EFFECT ON FLOW NEAR THE DELTA WING AT THE REGIME OF STRONG INTERACTION.pdf705.76KB
  • PDF2010 Volume 413TsAGI4103 (301-322) SOLUTION APPROACHES FOR FINITE-ELEMENT APPROXITION OF 3-D FLOWS.pdf819.64KB
  • PDF2010 Volume 413TsAGI4103 (323-340) GAS EJECTORS WITH TANGENTIAL BLOWING INTO THE MIXING CHAMBER.pdf739.85KB
  • PDF2010 Volume 413TsAGI4103 (341-356) STABILITY AND SELF-OSCILLATIONS OF NONLINEAR SINGLE-CIRCUIT AUTOTIC CONTROL SYSTEMS.pdf501.73KB
  • PDF2010 Volume 413TsAGI4103 (357-3) CALCULATION OF RADAR SIGNATURE CHARACTERISTICS OF THE ELEMENTS OF AIRCRAFT CONFIGURATION.pdf450.66KB
  • PDF2010 Volume 414TsAGI4104 (365-384) THEMATICAL MODEL OF THE AIRCRAFT AERODYNAMICS IN A VORTEXWAKE.pdf636.25KB
  • PDF2010 Volume 414TsAGI4104 (385-395) GROUP VELOCITY OF UNSTABLEWES IN A BOUNDARY LAYER AT SUPERSONIC SPEEDS.pdf308.51KB
  • PDF2010 Volume 414TsAGI4104 (397-408) INVESTIGATION OF PRE-SEPARATED FLOW IN AXISYMMETRICAL DIFFUSER.pdf269.67KB
  • PDF2010 Volume 414TsAGI4104 (409-421) NOZZLES WITH SHORT SUBSONIC CONTOURS AND A UNIFORM EXIT FLOW.pdf287.07KB
  • PDF2010 Volume 414TsAGI4104 (423-435) DIFFUSERS OF GAS-DYNAMIC LASERS - WAYS TO IMPROVE.pdf545.68KB
  • PDF2010 Volume 414TsAGI4104 (437-449) VORTEX FLOWS OF A MICROPOLAR FLUID.pdf314.71KB
  • PDF2010 Volume 414TsAGI4104 (451-471) OPTIMIZATION OF ARRANGEMENT OF PRESSURE GAGES USING A SIMULATION MODEL OF LOCAL FIELDS OF GAS-DYNAMIC PARAMETERS.pdf679.95KB
  • PDF2010 Volume 414TsAGI4104 (471-480) SIMULATION OF AIRCRAFT ABRUPT RESPONSE IN DIRECTIONAL CONTROL.pdf397.73KB
  • PDF2010 Volume 414TsAGI4104 (481-504) TECHNIQUE OF NUMERICAL EXPERIMENTS IN DESIGN CALCULATIONS OF HELICOPTER MECHANICAL SYSTEMS.pdf509.10KB
  • PDF2010 Volume 415TsAGI4105 (505-518) COMPUTATION OF IN ROTOR SE DUE TO BLADE THICKNESS.pdf1.90MB
  • PDF2010 Volume 415TsAGI4105 (519-529) PROSPECTS FOR REDUCTION IN SONIC BOOM LEVEL OF NEW-GENERATION COMMERCIAL SUPERSONIC PLANES.pdf609.84KB
  • PDF2010 Volume 415TsAGI4105 (531-533) TO THE THEORY OF KIRCHHOFF-TYPE POTENTIAL FLOWAROUND A BODY.pdf128.66KB
  • PDF2010 Volume 415TsAGI4105 (535-550) NUMERICAL SIMULATION OF THE AERODYNAMIC PERFORNCE OF A MICRO AIR VEHICLE.pdf704.12KB
  • PDF2010 Volume 415TsAGI4105 (551-566) AERODYNAMIC CHARACTERISTICS OF AN AIRCRAFT WITH A COMPLEX SHAPE TAKING INTO ACCOUNT THE POTENTIAL OF MOLECULAR FLOWINTERACTION WITH A SURFACE.pdf744.00KB
  • PDF2010 Volume 415TsAGI4105 (567-578) SELF-SIMILAR INTERPOLATION IN RAREFIED GAS DYNAMICS.pdf493.55KB
  • PDF2010 Volume 415TsAGI4105 (579-591) SOME DYNAMIC PROPERTIES OF DIGITAL MULTIRATE CONTROL SYSTEMS.pdf1.74MB
  • PDF2010 Volume 415TsAGI4105 (593-610) METHODS OF SOLVING THE EQUATION OF HELICOPTER ROTOR ELASTIC BLADE MOTION IN THE GENERAL CASE.pdf320.07KB
  • PDF2010 Volume 416TsAGI4106-001 CRITICAL AMPLITUDE OF THE TRELING PRESSURE WAVE CAUSING THE VORTEX SHEET FORTION IN THE BOUNDARY LAYER.pdf326.94KB
  • PDF2010 Volume 416TsAGI4106-002 INVESTIGATION OF THE TEMPERATURE FACTOR INFLUENCE ON HEAT TRANSFER OF A BLUNT BODY MODEL IN THE HIGH-SPEED GAS FLOW.pdf2.75MB
  • PDF2010 Volume 416TsAGI4106-003 3D SECONDARY SEPARATION AT SUPERSONIC FLOW OVER THE COMPRESSION RAMP.pdf2.92MB
  • PDF2010 Volume 416TsAGI4106-004 METHOD OF VISUALIZATION OF PULSATING TURBULENT FLOWS.pdf4.66MB
  • PDF2010 Volume 416TsAGI4106-005 ON THE ELECTROSTATIC PROBE THEORY FOR EMISSION OF PARTICLES FROM THE SURFACE.pdf228.72KB
  • PDF2010 Volume 416TsAGI4106-006 EVALUATION OF DIFFERENCES BETWEEN CHANNELS OF A DIGITAL CONTROL SYSTEM CAUSED BY CHANGES OF ITS VARIABLES.pdf1.28MB
  • PDF2010 Volume 416TsAGI4106-007 INFLUENCE OF ERRORS OF THE MUTUAL POSITION DETERMINATION OF REFUELING DROGUE AND REFUELING PROBE ON CONTACT ACCURACY AT AUTOTIC REFUELING.pdf619.01KB
  • PDF2010 Volume 416TSAGI4106-008 IMPACT OF CONTACT SHEAR STRESSES ON SERVICE LIFE OF CONNECTING ELEMENTS.pdf1.92MB
  • PDF2010 Volume 416TsAGI4106-009 TOWARD THE DEFINITION OF THE BOLT SHEARING LOAD IN MULTIPLE-ROW METAL COMPOSITE JOINTS.pdf3.28MB
  • PDF2011 Volume 421TsAGI4201-001-3438 EXPERIMENTAL INVESTIGATION OF THE SUPERSONIC BOUNDARY LAYER STABILITY ON A SWEPT WING AT CH NUMBER M = 2.pdf1.23MB
  • PDF2011 Volume 421TsAGI4201-002-3493 CIRCULAR CYLINDER IN THE TRANSONIC FLOWOF A VISCOUS PERFECT GAS.pdf3.55MB
  • PDF2011 Volume 421TsAGI4201-003-3439 DRAG OF CONE NOSES IN A SUPERSONIC FLOW.pdf605.07KB
  • PDF2011 Volume 421TsAGI4201-004-3437 FEATURES OF NUMERICAL MODELING OF A DIELECTRIC BARRIER DISCHARGE.pdf1.12MB
  • PDF2011 Volume 421TsAGI4201-005-3491 FACILITY FOR INVESTIGATIONS OF TOTAL HEMISPHERICAL EMISSIVITY OF HEAT PROTECTION TERIALS AND THERMAL CONTROL COATINGS.pdf463.69KB
  • PDF2011 Volume 421TsAGI4201-006-3490 DESCRIPTION OF RKOVIAN PROCESS DYNAMICS IN AN EXTENDED SPACE OF VARIABLES.pdf293.46KB
  • PDF2011 Volume 421TsAGI4201-007-3489 SYNTHESIS OF A SYNCHRONIZATION ALGORITHM FOR INTEGRATORS OF A DIGITAL REDUNDANT CONTROL SYSTEM.pdf878.25KB
  • PDF2011 Volume 421TsAGI4201-008-3495 APPLICATION OF THE MODEL OF VARIABLE DENSITY AT EARLY STAGES OF WING DESIGN.pdf651.82KB
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